EP2168001B1 - Microalignment using laser-softened glass bumps - Google Patents
Microalignment using laser-softened glass bumps Download PDFInfo
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- EP2168001B1 EP2168001B1 EP08794483A EP08794483A EP2168001B1 EP 2168001 B1 EP2168001 B1 EP 2168001B1 EP 08794483 A EP08794483 A EP 08794483A EP 08794483 A EP08794483 A EP 08794483A EP 2168001 B1 EP2168001 B1 EP 2168001B1
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- substrate
- bumps
- glass
- bump
- oversized
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- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/24—Coupling light guides
- G02B6/42—Coupling light guides with opto-electronic elements
- G02B6/4201—Packages, e.g. shape, construction, internal or external details
- G02B6/4219—Mechanical fixtures for holding or positioning the elements relative to each other in the couplings; Alignment methods for the elements, e.g. measuring or observing methods especially used therefor
- G02B6/422—Active alignment, i.e. moving the elements in response to the detected degree of coupling or position of the elements
- G02B6/4226—Positioning means for moving the elements into alignment, e.g. alignment screws, deformation of the mount
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- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B23/00—Re-forming shaped glass
- C03B23/0013—Re-forming shaped glass by pressing
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B23/00—Re-forming shaped glass
- C03B23/02—Re-forming glass sheets
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B23/00—Re-forming shaped glass
- C03B23/02—Re-forming glass sheets
- C03B23/023—Re-forming glass sheets by bending
- C03B23/03—Re-forming glass sheets by bending by press-bending between shaping moulds
- C03B23/0307—Press-bending involving applying local or additional heating, cooling or insulating means
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C19/00—Surface treatment of glass, not in the form of fibres or filaments, by mechanical means
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C23/00—Other surface treatment of glass not in the form of fibres or filaments
- C03C23/0005—Other surface treatment of glass not in the form of fibres or filaments by irradiation
- C03C23/0025—Other surface treatment of glass not in the form of fibres or filaments by irradiation by a laser beam
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C23/00—Other surface treatment of glass not in the form of fibres or filaments
- C03C23/007—Other surface treatment of glass not in the form of fibres or filaments by thermal treatment
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/24—Coupling light guides
- G02B6/26—Optical coupling means
- G02B6/30—Optical coupling means for use between fibre and thin-film device
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/24—Coupling light guides
- G02B6/42—Coupling light guides with opto-electronic elements
- G02B6/4201—Packages, e.g. shape, construction, internal or external details
- G02B6/4219—Mechanical fixtures for holding or positioning the elements relative to each other in the couplings; Alignment methods for the elements, e.g. measuring or observing methods especially used therefor
- G02B6/4228—Passive alignment, i.e. without a detection of the degree of coupling or the position of the elements
- G02B6/4232—Passive alignment, i.e. without a detection of the degree of coupling or the position of the elements using the surface tension of fluid solder to align the elements, e.g. solder bump techniques
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B6/00—Light guides; Structural details of arrangements comprising light guides and other optical elements, e.g. couplings
- G02B6/24—Coupling light guides
- G02B6/42—Coupling light guides with opto-electronic elements
- G02B6/4201—Packages, e.g. shape, construction, internal or external details
- G02B6/4219—Mechanical fixtures for holding or positioning the elements relative to each other in the couplings; Alignment methods for the elements, e.g. measuring or observing methods especially used therefor
- G02B6/4234—Passive alignment along the optical axis and active alignment perpendicular to the optical axis
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B7/00—Mountings, adjusting means, or light-tight connections, for optical elements
- G02B7/003—Alignment of optical elements
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03B—MANUFACTURE, SHAPING, OR SUPPLEMENTARY PROCESSES
- C03B2215/00—Press-moulding glass
- C03B2215/40—Product characteristics
- C03B2215/41—Profiled surfaces
- C03B2215/414—Arrays of products, e.g. lenses
-
- C—CHEMISTRY; METALLURGY
- C03—GLASS; MINERAL OR SLAG WOOL
- C03C—CHEMICAL COMPOSITION OF GLASSES, GLAZES OR VITREOUS ENAMELS; SURFACE TREATMENT OF GLASS; SURFACE TREATMENT OF FIBRES OR FILAMENTS MADE FROM GLASS, MINERALS OR SLAGS; JOINING GLASS TO GLASS OR OTHER MATERIALS
- C03C2204/00—Glasses, glazes or enamels with special properties
- C03C2204/08—Glass having a rough surface
Definitions
- This Invention relates in general to microalignment of two or more bodies, and in particular to microalignment of planar substrates using time-of-assembly electro-thermal actuation.
- Planar waveguide device alignment is typically provided by an external precision positioning system such as multi-axis translation/rotation stages driven by piezo-electric micropositioners, for example.
- An attachment material such as an organic adhesive or metallic solder is generally positioned between aligned substrates and used to maintain long-term substrate alignment. While precision positioning systems can generally align waveguide arrays on two planar waveguide devices to within less than 0.2 ⁇ m lateral misalignment, a critical issue is maintaining waveguide alignment during adhesive curing without high rates of post-attachment rework.
- Crystal block attachment such as disclosed in U.S. Patent No. 6,512,642 "Method and structure for aligning optical elements", assigned to the owner of the present application, is one solution for zero-shift attachment of devices to substrates, but the cantilever nature of the planar device attachment to the common alignment substrate via an intermediate block makes the approach less suitable for planar devices requiring wirebonded electrical interconnections. Additionally, a full six-axis positioning system is required to align the two substrates.
- An alternative planar device alignment and attachment approach involves microactuators that are integrated into or mounted on the common alignment substrate.
- integrated micro actuators have been previously described that are based on expansion and/or contraction of piezoelectric materials, electro-strictive materials, magnetostrictive materials and magnetic materials.
- Microactuators have also been fabricated based on electrostatic forces between plates and substrates, electrically-induced shape changes in polymers and ultrasonic excitation of flexure elements.
- Another common integrated microactuator approach takes advantage of material expansion and/or contraction via the thermo-mechanical effect.
- microactuator structures which are often integrated into planar substrates using MEMS and semiconductor fabrication processes, can be broadly categorized into two groups: (1) Microactuators based on heating of selected supporting arms or beams, where the arms or beams are fabricated using a single material. Since remaining arms, beams or supporting structures are unheated, CTE-induced differential forces on the arms or beams lead to deformation (translation and/or rotation) of the microactuator structure; (2) Microactuators that deform because supporting arms are bi-material laminates fabricated from materials with two different CTEs. When these arms are heated, they provide actuation by curving toward the lower-CTE material.
- MEMS complex precision microstructures
- thermo-mechanical actuator can be formed by heating a polymer material in an enclosed cavity so that when it expands a force is exerted in a predefined direction.
- This actuator solution is relatively simple compared to MEMS actuator approaches, but constant application of control input (e.g., electric potential for a polymer heater) is still required. Also, since actuation is provided by thermo-mechanical polymer expansion, changes in ambient temperature could induce changes in polymer size, resulting in unwanted shifts in actuator position.
- a family of IR-absorbing Pyrex TM -like glasses was recently developed at Corning. This process enables dark glass bump formation for bump heights of up to 70-100 ⁇ m. These bumps can be used as standoff structures for alignment of planar waveguide device substrate.
- One or more laser heating cycles direct energy to the bump to increase its height.
- the bump height can be slowly increased until a target height is reached.
- JP 10 214859 A discloses a method for fabricating bump standoff structures according to the preamble of claim 1.
- An embodiment of this Invention includes a technique for fabricating glass bump standoff structures of precise height by (1) forming oversized glass bumps and (2) slowly reducing the height of these bumps via the combination of controlled bump softening and downward pressure applied on a cover substrate.
- Lasers are used preferentially to soften the bumps, but other energy sources may be used.
- the laser wavelength selected for bump softening preferably allows the beam to pass through the cover substrate with minimal optical absorption. For example, light from a 1.55 ⁇ m laser will pass through a Si substrate with minimal absorption but experiences relatively strong absorption and local heating in absorptive glasses, such as, for example, Fe and Cu-doped glasses (hereinafter "dark" glass).
- oversized dark glass bumps can be formed in-situ using laser formation or prior to dark glass substrate mounting via a variety of low-cost processes (e.g., embossing, molding); improved process control can be achieved for accurate cover substrate height positioning by use of multiple process parameters (variable laser power and cover substrate applied pressure, for example); the cover substrate height may be able to be re-positioned, after initial alignment, by repeating the bump laser heating and substrate alignment operations; cover substrate thermally insulating coating layers or surface structures can function to limit thermal dissipation through the cover substrate during bump softening; the bump softening process creates support structures with enlarged contact areas that provide improved mechanical support for the cover substrate, especially if the initial bump formation process results in bump weakening via microcracking; the same IR laser used in bump softening can also be used to locally cure adhesives placed between the cover substrate and the dark glass substrate.
- Figure 1 is a diagrammatic cross section of a hybrid assembly or portion thereof according to one aspect of the present invention.
- Figure 2 is a diagrammatic cross section of the hybrid assembly of Figure 1 with a planar waveguide substrate 14 positioned thereon for alignment to another substrate in the form of an SOA 18.
- Figure 3 is a diagrammatic cross section of the hybrid assembly of Figure 2 showing irradiation by an irradiation beam 36 from a source 38.
- Figure 4 is a diagrammatic cross section of the hybrid assembly of Figure 3 showing softening and resulting reduction in height of bump 28a.
- Figure 5 is a diagrammatic cross section of the hybrid assembly of Figure 4 showing softening and resulting reduction in height of bump 28b.
- Figure 6 is a diagrammatic cross section of the hybrid assembly of Figure 5 after completion of alignment of waveguides 16 with waveguides 12, showing the relatively large contact area 29 between bumps 28 and substrate 14.
- Figure 1 shows a hybrid assembly 10 wherein optical waveguides 12 on a planar waveguide substrate 14 (both shown in Figure 2 ) must be aligned to waveguides 16 on an SOA (Semiconductor Optical Amplifier) array substrate 18.
- the waveguides 12 and waveguides 16 are shown in a cross section in which only a single representative waveguide 12 is visible, with multiple waveguides positioned below and above the plane of the Figures.
- a dark glass substrate 20 is mounted on a lower alignment substrate 22 using an organic adhesive or solder 24.
- the SOA array substrate 18 is also mounted on the alignment substrate 22 by any acceptable method such as a solder layer 26.
- the dark glass substrate 20 provides oversized glass bumps 28 that will later serve as alignment standoffs. The bumps are termed "oversized" because they have a height or standoff distance 30 from the dark glass substrate 20 which is greater than necessary to be to properly align waveguides 12 on the planar waveguide substrate 14 to the SOA array waveguides 16.
- the oversized dark glass bumps 28 desirably can be created in situ (on the substrate 20 during the assembly and alignment process of the hybrid assembly 10) using laser bump formation.
- the bumps can also be pre-fabricated on the dark glass substrate 20 prior to attachment of the substrate 20 to the alignment substrate 22.
- Height tolerance for the oversized bumps may be relatively relaxed (for example, as great as 5-30 ⁇ m), since subsequent alignment steps will accomplish fine height alignment (for example, to tolerances of 0.1-0.3 ⁇ m).
- the relaxed bump height requirement enables a wide array of low-cost bump pre-fabrication processes, including but not limited to laser bump formation, molding, embossing, surface machining or frit screen printing.
- oversized glass bumps 28 for use in the context of the present invention may be formed by hot embossing a thin sheet of glass to form a series of closely-spaced raised domes.
- a planar waveguide substrate such as planar waveguide substrate 14 connected to an optical fiber 32 by a pigtail block 34, is then positioned on top of the oversized glass bumps 28 as shown in Figure 2 .
- the planar waveguide substrate waveguides 12 are roughly aligned to the SOA array waveguides 16. Due to the oversized glass bumps, the planar waveguide substrate waveguides are displaced vertically from the SOA array waveguides by a relatively small distance, for example, 5-30 ⁇ m.
- a radiation beam 36 such as an IR radiation beam from a suitable source 38, such as a 1550 nm laser, is then directed through the planar waveguide substrate 14 and onto an oversized dark glass bump, such as bump 28a, as shown in Figure 3 .
- Si planar waveguide substrate with relatively little attenuation, for example.
- This same light is strongly absorbed as it passed through the dark glass substrate 20, leading to dark glass bump heating in Figure 3 .
- Figure 3 shows the radiation beam 36 passing through the planar waveguide substrate 14 from the top, but in an alternative configuration of dark glass bump heating could be accomplished using IR radiation from below.
- This approach would require the lower alignment substrate 22 to be fabricated in a material that is transparent to IR radiation (e.g., Si or silica).
- optional heater electrodes 40 directly on or near the dark glass bumps may provide IR radiation for bump heating. These heater electrodes 40 could also be positioned on neighboring substrates in close proximity to the dark glass bumps, such as the planar waveguide substrate 14 or the alignment substrate 22.
- the downward pressure is applied to the top surface of the planar waveguide substrate 14, as indicated generally by the solid arrow 42. If the oversized dark glass bump 28a is heated sufficiently, the downward pressure 42 will gradually reduce the height of the dark glass bump 28a and cause the glass of the bump 28a (the "bump glass") to be displaced laterally, as shown in Figure 4 .
- the rate of bump height reduction can be controlled by adjusting the pressure applied to the planar waveguide substrate 14 and/or the beam power of the radiation beam 36 applied to the dark glass bump 28.
- the dark glass bump heating process is repeated for the remaining oversized bump(s) 28b, as shown in Figure 5 .
- the planar waveguide substrate waveguides 12 can be aligned to the SOA array substrate waveguides 16, as shown in Figure 6 .
- This dark glass bump-based substrate alignment process may be significantly advantaged over other dark glass alignment approaches because a mechanical contact area 29 at the top of the dark glass bump 28, between the glass bump 28 and the plan waveguide substrate 14, can be made relatively large.
- This larger contact area 29 provides increased bump strength and resistance to deformation during alignment and adhesive under-fill cure processes.
- This larger contact area may be particularly important if microcracking or other structural defects significantly weaken other laser-formed dark glass bumps.
- pre-fabricated dark glass bump forming processes such as embossing, molding and so forth, arbitrarily shaped oversize bump shapes can be made, including shapes with larger substrate contact areas, if desired.
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Description
- This Invention relates in general to microalignment of two or more bodies, and in particular to microalignment of planar substrates using time-of-assembly electro-thermal actuation.
- Planar waveguide device alignment is typically provided by an external precision positioning system such as multi-axis translation/rotation stages driven by piezo-electric micropositioners, for example. An attachment material such as an organic adhesive or metallic solder is generally positioned between aligned substrates and used to maintain long-term substrate alignment. While precision positioning systems can generally align waveguide arrays on two planar waveguide devices to within less than 0.2 µm lateral misalignment, a critical issue is maintaining waveguide alignment during adhesive curing without high rates of post-attachment rework.
- In laser welding applications, post-weld bending rework is often required to achieve sub-micron lateral alignment of single waveguides. Using this method to align arrays of planar waveguides is more difficult when the bending rotation occurs in the plane parallel to the planar substrate: the rotation introduces a gap at one end of the waveguide array, introducing unwanted axial misalignments and coupling losses.
- Crystal block attachment, such as disclosed in
U.S. Patent No. 6,512,642 "Method and structure for aligning optical elements", assigned to the owner of the present application, is one solution for zero-shift attachment of devices to substrates, but the cantilever nature of the planar device attachment to the common alignment substrate via an intermediate block makes the approach less suitable for planar devices requiring wirebonded electrical interconnections. Additionally, a full six-axis positioning system is required to align the two substrates. - An alternative planar device alignment and attachment approach involves microactuators that are integrated into or mounted on the common alignment substrate. For example, integrated micro actuators have been previously described that are based on expansion and/or contraction of piezoelectric materials, electro-strictive materials, magnetostrictive materials and magnetic materials. Microactuators have also been fabricated based on electrostatic forces between plates and substrates, electrically-induced shape changes in polymers and ultrasonic excitation of flexure elements. Another common integrated microactuator approach takes advantage of material expansion and/or contraction via the thermo-mechanical effect. These microactuator structures, which are often integrated into planar substrates using MEMS and semiconductor fabrication processes, can be broadly categorized into two groups: (1) Microactuators based on heating of selected supporting arms or beams, where the arms or beams are fabricated using a single material. Since remaining arms, beams or supporting structures are unheated, CTE-induced differential forces on the arms or beams lead to deformation (translation and/or rotation) of the microactuator structure; (2) Microactuators that deform because supporting arms are bi-material laminates fabricated from materials with two different CTEs. When these arms are heated, they provide actuation by curving toward the lower-CTE material.
- A disadvantage with all of these actuation approaches is that they require continuous control input (e.g., an electrical signal) in order to maintain their position. This is a significant disadvantage in microalignment of hybrid optical components, since it means this control input must be maintained over the life of the product. Further, many of the microalignment technologies described above require complex precision microstructures (MEMS, for example) that increase product cost. MEMS actuators can be designed with integrated latch structures so that their position is maintained after the control input is removed. Yet these actuators can be expected to be even more complex in design than standard MEMS mentioned, resulting in even higher product cost.
- Another type of thermo-mechanical actuator can be formed by heating a polymer material in an enclosed cavity so that when it expands a force is exerted in a predefined direction. This actuator solution is relatively simple compared to MEMS actuator approaches, but constant application of control input (e.g., electric potential for a polymer heater) is still required. Also, since actuation is provided by thermo-mechanical polymer expansion, changes in ambient temperature could induce changes in polymer size, resulting in unwanted shifts in actuator position.
- A family of IR-absorbing Pyrex™-like glasses was recently developed at Corning. This process enables dark glass bump formation for bump heights of up to 70-100 µm. These bumps can be used as standoff structures for alignment of planar waveguide device substrate. One or more laser heating cycles direct energy to the bump to increase its height. Using a closed-loop control system, the bump height can be slowly increased until a target height is reached.
-
discloses a method for fabricating bump standoff structures according to the preamble of claim 1.JP 10 214859 A - An embodiment of this Invention includes a technique for fabricating glass bump standoff structures of precise height by (1) forming oversized glass bumps and (2) slowly reducing the height of these bumps via the combination of controlled bump softening and downward pressure applied on a cover substrate. Lasers are used preferentially to soften the bumps, but other energy sources may be used. The laser wavelength selected for bump softening preferably allows the beam to pass through the cover substrate with minimal optical absorption. For example, light from a 1.55 µm laser will pass through a Si substrate with minimal absorption but experiences relatively strong absorption and local heating in absorptive glasses, such as, for example, Fe and Cu-doped glasses (hereinafter "dark" glass).
- According to various embodiments of the methods and techniques of the present invention: oversized dark glass bumps can be formed in-situ using laser formation or prior to dark glass substrate mounting via a variety of low-cost processes (e.g., embossing, molding); improved process control can be achieved for accurate cover substrate height positioning by use of multiple process parameters (variable laser power and cover substrate applied pressure, for example); the cover substrate height may be able to be re-positioned, after initial alignment, by repeating the bump laser heating and substrate alignment operations; cover substrate thermally insulating coating layers or surface structures can function to limit thermal dissipation through the cover substrate during bump softening; the bump softening process creates support structures with enlarged contact areas that provide improved mechanical support for the cover substrate, especially if the initial bump formation process results in bump weakening via microcracking; the same IR laser used in bump softening can also be used to locally cure adhesives placed between the cover substrate and the dark glass substrate. Other features and advantages will be apparent from the remainder of the description and the related drawings.
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Figure 1 is a diagrammatic cross section of a hybrid assembly or portion thereof according to one aspect of the present invention. -
Figure 2 is a diagrammatic cross section of the hybrid assembly ofFigure 1 with aplanar waveguide substrate 14 positioned thereon for alignment to another substrate in the form of anSOA 18. -
Figure 3 is a diagrammatic cross section of the hybrid assembly ofFigure 2 showing irradiation by anirradiation beam 36 from asource 38. -
Figure 4 is a diagrammatic cross section of the hybrid assembly ofFigure 3 showing softening and resulting reduction in height ofbump 28a. -
Figure 5 is a diagrammatic cross section of the hybrid assembly ofFigure 4 showing softening and resulting reduction in height ofbump 28b. -
Figure 6 is a diagrammatic cross section of the hybrid assembly ofFigure 5 after completion of alignment ofwaveguides 16 withwaveguides 12, showing the relativelylarge contact area 29 betweenbumps 28 andsubstrate 14. -
Figure 1 shows ahybrid assembly 10 whereinoptical waveguides 12 on a planar waveguide substrate 14 (both shown inFigure 2 ) must be aligned to waveguides 16 on an SOA (Semiconductor Optical Amplifier)array substrate 18. (Thewaveguides 12 andwaveguides 16 are shown in a cross section in which only a singlerepresentative waveguide 12 is visible, with multiple waveguides positioned below and above the plane of the Figures.) Adark glass substrate 20 is mounted on alower alignment substrate 22 using an organic adhesive orsolder 24. TheSOA array substrate 18 is also mounted on thealignment substrate 22 by any acceptable method such as asolder layer 26. Thedark glass substrate 20 providesoversized glass bumps 28 that will later serve as alignment standoffs. The bumps are termed "oversized" because they have a height orstandoff distance 30 from thedark glass substrate 20 which is greater than necessary to be to properly alignwaveguides 12 on theplanar waveguide substrate 14 to theSOA array waveguides 16. - The oversized
dark glass bumps 28 desirably can be created in situ (on thesubstrate 20 during the assembly and alignment process of the hybrid assembly 10) using laser bump formation. The bumps can also be pre-fabricated on thedark glass substrate 20 prior to attachment of thesubstrate 20 to thealignment substrate 22. Height tolerance for the oversized bumps may be relatively relaxed (for example, as great as 5-30µm), since subsequent alignment steps will accomplish fine height alignment (for example, to tolerances of 0.1-0.3 µm). The relaxed bump height requirement enables a wide array of low-cost bump pre-fabrication processes, including but not limited to laser bump formation, molding, embossing, surface machining or frit screen printing. For example,oversized glass bumps 28 for use in the context of the present invention may be formed by hot embossing a thin sheet of glass to form a series of closely-spaced raised domes. - A planar waveguide substrate, such as
planar waveguide substrate 14 connected to anoptical fiber 32 by apigtail block 34, is then positioned on top of theoversized glass bumps 28 as shown inFigure 2 . Using top-side visible or IR imaging, the planarwaveguide substrate waveguides 12 are roughly aligned to theSOA array waveguides 16. Due to the oversized glass bumps, the planar waveguide substrate waveguides are displaced vertically from the SOA array waveguides by a relatively small distance, for example, 5-30 µm. - A
radiation beam 36, such as an IR radiation beam from asuitable source 38, such as a 1550 nm laser, is then directed through theplanar waveguide substrate 14 and onto an oversized dark glass bump, such asbump 28a, as shown inFigure 3 . Long wavelength IR light (e.g. λ = 1.55 µm) will pass through a Si planar waveguide substrate with relatively little attenuation, for example. This same light, however, is strongly absorbed as it passed through thedark glass substrate 20, leading to dark glass bump heating inFigure 3 . If theplanar waveguide substrate 14 is fabricated in silica instead of Si, a shorter wavelength source (e.g., λ = 850 nm) may be used. -
Figure 3 shows theradiation beam 36 passing through theplanar waveguide substrate 14 from the top, but in an alternative configuration of dark glass bump heating could be accomplished using IR radiation from below. This approach would require thelower alignment substrate 22 to be fabricated in a material that is transparent to IR radiation (e.g., Si or silica). In another optional approach,optional heater electrodes 40 directly on or near the dark glass bumps may provide IR radiation for bump heating. Theseheater electrodes 40 could also be positioned on neighboring substrates in close proximity to the dark glass bumps, such as theplanar waveguide substrate 14 or thealignment substrate 22. - During the dark glass heating process, downward pressure is applied to the top surface of the
planar waveguide substrate 14, as indicated generally by thesolid arrow 42. If the oversizeddark glass bump 28a is heated sufficiently, thedownward pressure 42 will gradually reduce the height of thedark glass bump 28a and cause the glass of thebump 28a (the "bump glass") to be displaced laterally, as shown inFigure 4 . The rate of bump height reduction can be controlled by adjusting the pressure applied to theplanar waveguide substrate 14 and/or the beam power of theradiation beam 36 applied to thedark glass bump 28. - The dark glass bump heating process is repeated for the remaining oversized bump(s) 28b, as shown in
Figure 5 . By gradually reducing the height of the oversized bumps 28 (for example, by multiple heating cycles on multiple bumps 28) the planarwaveguide substrate waveguides 12 can be aligned to the SOAarray substrate waveguides 16, as shown inFigure 6 . - This dark glass bump-based substrate alignment process may be significantly advantaged over other dark glass alignment approaches because a
mechanical contact area 29 at the top of thedark glass bump 28, between theglass bump 28 and theplan waveguide substrate 14, can be made relatively large. Thislarger contact area 29 provides increased bump strength and resistance to deformation during alignment and adhesive under-fill cure processes. This larger contact area may be particularly important if microcracking or other structural defects significantly weaken other laser-formed dark glass bumps. Using pre-fabricated dark glass bump forming processes such as embossing, molding and so forth, arbitrarily shaped oversize bump shapes can be made, including shapes with larger substrate contact areas, if desired.
Claims (9)
- A method for fabricating bump standoff structures of precise height, the method comprising:providing oversized bumps (28);providing a heat source (38) to heat the bumps (28);providing a substrate (14) to be aligned;reducing the height of the oversized bumps (28) by a combination of manipulations comprising (a) softening the bumps (28) by heating the bumps (28) and (b) applying pressure to the substrate (14) to be aligned;characterized in thatsaid oversized bumps (28) are made of glass and are provided on a glass substrate (20); andsaid substrate (14) to be aligned is positioned on said oversized glass bumps (28).
- The method according to claim 1, wherein the heat source (38) is an irradiation beam (36) in combination with the glass substrate (20) being absorbing at a wavelength of the irradiation beam.
- The method according to claim 2, wherein the irradiation beam (36) is a laser.
- The method according to either of claims 2 and 3, wherein the irradiation beam (36) is a 1.55 µm laser.
- The method according to any of claims 1-4, wherein the substrate (14) to be aligned comprises silicon.
- The method according to any of claims 1-5, wherein the step of reducing the bump height includes irradiating the bumps (28) through the substrate (14) to be aligned.
- The method according to any of claims 1-5, wherein the method further comprises positioning the glass substrate (20) on an alignment substrate (22), and the step of reducing the bump height includes irradiating the bumps (28) through the alignment substrate (22).
- The method according to any of claims 1-7, wherein the step of providing oversized glass bumps (28) on a glass substrate (20) comprises embossing or molding glass bumps (289 on the glass substrate (20).
- The method according to any of claims 1-7, wherein the step of providing oversized glass bumps (28) on a glass substrate (20) comprises irradiating the glass substrate (20) with a laser.
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US95964007P | 2007-07-16 | 2007-07-16 | |
| US505507P | 2007-11-30 | 2007-11-30 | |
| PCT/US2008/008609 WO2009011834A2 (en) | 2007-07-16 | 2008-07-15 | Microalignment using laser-softened glass bumps |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| EP2168001A2 EP2168001A2 (en) | 2010-03-31 |
| EP2168001B1 true EP2168001B1 (en) | 2013-03-06 |
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| EP08794483A Not-in-force EP2168001B1 (en) | 2007-07-16 | 2008-07-15 | Microalignment using laser-softened glass bumps |
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| US (1) | US8291729B2 (en) |
| EP (1) | EP2168001B1 (en) |
| JP (1) | JP5378376B2 (en) |
| TW (1) | TWI400499B (en) |
| WO (1) | WO2009011834A2 (en) |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8821999B2 (en) * | 2008-11-05 | 2014-09-02 | Corning Incorporated | Vacuum-insulated glass windows with glass-bump spacers |
| US8679599B2 (en) * | 2011-03-29 | 2014-03-25 | Corning Incorporated | Light-weight strengthened, low-emittance vacuum insulated glass (VIG) windows |
| US9346710B2 (en) * | 2012-05-29 | 2016-05-24 | Corning Incorporated | Sheet glass product fabrication with growth-limited glass bump spacers |
| US8904822B2 (en) * | 2012-11-06 | 2014-12-09 | Corning Incorporated | Thickness control of substrates |
| JP2016106237A (en) * | 2013-03-25 | 2016-06-16 | 技術研究組合光電子融合基盤技術研究所 | Optical module and optical module production method |
| JP6147689B2 (en) * | 2014-03-05 | 2017-06-14 | 株式会社東芝 | MEMS equipment |
| ES2590538B1 (en) * | 2015-05-22 | 2017-10-19 | Bsh Electrodomésticos España, S.A. | PROCEDURE FOR THE MANUFACTURE OF A COOKING FIELD PLATE, AND COOKING FIELD PLATE |
| US9359252B1 (en) | 2015-07-24 | 2016-06-07 | Corning Incorporated | Methods for controlled laser-induced growth of glass bumps on glass articles |
| US10336644B2 (en) | 2016-05-26 | 2019-07-02 | Corning Optical Communication Llc | Methods of ferrule reshaping for correcting core-to-ferrule concentricity errors, and optical fiber cable assemblies related to such methods |
| US11420293B2 (en) | 2016-05-26 | 2022-08-23 | Corning Optical Communications LLC | Methods of ferrule reshaping for correcting core-to-ferrule concentricity errors, and optical fiber cable assemblies related to such methods |
| US10180544B2 (en) | 2016-11-17 | 2019-01-15 | Corning Optical Communications LLC | Micro-optical systems and assemblies using glass tubes and methods of forming same |
| EP3541764A1 (en) * | 2016-11-18 | 2019-09-25 | Corning Incorporated | Methods of forming laser-induced attributes on glass-based substrates using mid-ir laser |
| US10578811B2 (en) | 2017-11-29 | 2020-03-03 | Corning Optical Communications LLC | Methods of forming ferrules for optical fiber connectors, and optical fiber cable assemblies related to such methods |
| US10663660B2 (en) * | 2018-01-25 | 2020-05-26 | Poet Technologies, Inc. | Optical dielectric waveguide subassembly structures |
| US11768334B2 (en) | 2021-06-24 | 2023-09-26 | Corning Research & Development Corporation | Lensed optical fiber connector with dust insensitive alignment features |
| US12394690B2 (en) | 2022-01-04 | 2025-08-19 | Corning Research & Development Corporation | Systems and methods of nano-particle bonding for electronics cooling |
Family Cites Families (16)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH02139944A (en) * | 1988-11-18 | 1990-05-29 | Omron Tateisi Electron Co | Mounting of semiconductor chip |
| US5766053A (en) * | 1995-02-10 | 1998-06-16 | Micron Technology, Inc. | Internal plate flat-panel field emission display |
| US5720169A (en) * | 1995-05-23 | 1998-02-24 | Schneider; Edward T. | Thermochemical/mechanical actuator |
| US6124663A (en) * | 1996-12-16 | 2000-09-26 | The Boeing Company | Fiber optic connector having a microelectromechanical positioning apparatus and an associated fabrication method |
| JPH10214859A (en) * | 1997-01-28 | 1998-08-11 | Taiyo Yuden Co Ltd | Manufacture of circuit module |
| FR2779536B1 (en) * | 1998-06-09 | 2001-10-19 | Commissariat Energie Atomique | ASSEMBLY FOR CONNECTING OPTICAL FIBERS WITH OPTICAL OR OPTOELECTRONIC COMPONENTS AND METHOD OF MANUFACTURING SUCH ASSEMBLY |
| DE19936863A1 (en) * | 1999-08-05 | 2001-02-15 | Patent Treuhand Ges Fuer Elektrische Gluehlampen Mbh | Manufacturing process for a gas discharge lamp |
| US6391213B1 (en) * | 1999-09-07 | 2002-05-21 | Komag, Inc. | Texturing of a landing zone on glass-based substrates by a chemical etching process |
| SG108260A1 (en) * | 2001-06-29 | 2005-01-28 | Inst Data Storage | Flat panel display and method of manufacture |
| US6512642B1 (en) * | 2001-07-10 | 2003-01-28 | Corning Incorporated | Method and structure for aligning optical elements |
| WO2003058286A2 (en) * | 2002-01-10 | 2003-07-17 | Galayor Networks Inc. | Monolithic optical control components |
| US20050116245A1 (en) * | 2003-04-16 | 2005-06-02 | Aitken Bruce G. | Hermetically sealed glass package and method of fabrication |
| TW200631151A (en) | 2005-02-24 | 2006-09-01 | Jet Tech Ltd | Apparatus and method for bonding anisotropic conductive film using laser beam |
| US20060196600A1 (en) * | 2005-03-03 | 2006-09-07 | Gi-Jung Nam | Apparatus and method for bonding anisotropic conductive film using laser beam |
| US7480432B2 (en) * | 2006-02-28 | 2009-01-20 | Corning Incorporated | Glass-based micropositioning systems and methods |
| JP2007305737A (en) * | 2006-05-10 | 2007-11-22 | Seiko Epson Corp | Manufacturing method of optical module |
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2008
- 2008-07-15 TW TW097126875A patent/TWI400499B/en not_active IP Right Cessation
- 2008-07-15 US US12/669,365 patent/US8291729B2/en not_active Expired - Fee Related
- 2008-07-15 WO PCT/US2008/008609 patent/WO2009011834A2/en not_active Ceased
- 2008-07-15 EP EP08794483A patent/EP2168001B1/en not_active Not-in-force
- 2008-07-15 JP JP2010517002A patent/JP5378376B2/en not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| WO2009011834A3 (en) | 2009-03-05 |
| US20100206006A1 (en) | 2010-08-19 |
| US8291729B2 (en) | 2012-10-23 |
| EP2168001A2 (en) | 2010-03-31 |
| JP2010533891A (en) | 2010-10-28 |
| TW200933229A (en) | 2009-08-01 |
| TWI400499B (en) | 2013-07-01 |
| WO2009011834A2 (en) | 2009-01-22 |
| JP5378376B2 (en) | 2013-12-25 |
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